Download
1 / 19
190 likes | 202 Views
Constellation-X Mirror Development: Achievements, Problems, and Prospects. Will Zhang Laboratory for X-Ray Astrophysics NASA Goddard Space Flight Center. Mirror Development Team. GSFC: David Content John Lehan Rob Petre Timo Saha Will Zhang. MSFC: Bill Jones Mikhail Gubarev
E N D
Constellation-X Mirror Development: Achievements, Problems, and Prospects Will Zhang Laboratory for X-Ray Astrophysics NASA Goddard Space Flight Center
Mirror Development Team GSFC: David Content John Lehan Rob Petre Timo Saha Will Zhang MSFC: Bill Jones Mikhail Gubarev Steve O’Dell Technology Development Manager: Scott Owens Laboratory Manager: Curtis Odell Technical Support: James Mazzarella, Marton Sharpe, Melinda Hong, John Kearney SAO: Paul Reid
Fabrication Metrology • Mirror segment held at 3 points • 25 axial scans for each mirror, one every 2 degrees • Verification of the fabrication process • Feedback to the fabrication process • Start with a sheet of commercially available borosilicate glass, 0.4mm thick • Place it on a fused quartz mandrel whose surface has been treated to prevent sticking and provide other necessary properties for slumping • Start a temperature cycle between between 20 and 600 degrees C Goal: Make every mirror look exactly like the mandrel and prove it
Development Strategy • Start with a technique that meets three (effective area, mass, and production cost) of thefour requirements, work on the fourth one (angular resolution) • Pursue reproducibility, or process determinism: making all the mirrors look alike • Pursue traceability: making all the mirrors look like the mandrels
Apparent Surface Map(including both fabrication error and gravity distortion)
Distribution of Apparent Mirror Quality(all mirrors produced between Jan and Apr 2006)
Repeatability: Slumping is a deterministic process Necessary Conditions to Have Repeatability • Forming has to be good • Metrology registration has to be good • Distortion has to be very small or nearly identical Best: 21nm RMS Typical: 50nm RMS These numbers are most likely dominated by a lack of accurate cross registration, therefore should be considered as upper limits
Comparison between Mandrel and MirrorBlack=Mirror; Blue=Mandrel
Result from a new mirror support Mandrel Black: with new support Blue: with 3-point support
Error Decomposition Estimate Easy to solve Relatively easy No. 1 Issue Potential of this technology
Summary of Status and Issus • We have achieved excellent repeatability in slumping substrates • Typical: 50nm RMS • Best: 20nm RMS • These mirrors, when properly integrated, are expected to perform better than 20 arcsec (HPD, 2 reflections) • We need to address the following issues • Metrology • Use better reference optics: commission of a new 10-in interferometer • Construct better mirror holding fixture: mattress • Understand, reduce/eliminate the mid-frequency error
Mid-frequency Problem and Its Solution • Cause: dust from the slumping environment and detritus resulting from the release layer • Solution: • Better slumping environment: clean oven • Improved mandrel surface release layer
Prospects • Almost all technological aspects of the mirror fabrication are understood and going very well: • Problems are well defined • Solutions are being implemented • In all likelihood, we will be able to do significantly better than the SXT baseline requirements. By the end of this year we should be able to quantitatively gauge • whether the present technology can achieve the SXT goal of 5 arcsec • What specific things we need to do to reach the goal
AcknowledgementsThis work has been supported in part byThe Constellation-X Project OfficeGSFC Core Competence FundA NASA Astronomy and Physics Analysis GrantGSFC Internal R&D FundGSFC Technical Equipment FundGSFC Director’s Discretionary Fund
SXT Mandrel Challenge in Perspective • Manufacture of SXT mandrels is NOT challenging in historic terms. • Comparable to, or easier than, XMM’s mandrels because of smaller area • Much easier than Chandra’s mirrors because of much less stringent figure requirements • Much easier than JWST mirrors because there are no lightweighting or cryogenic requirements
Mirror Segment Description Interferometer Coordinate Measuring Machine By definition/convention, all the Delta terms (azimuth dependent) have zero means. So does also the R(z,phi) term.
